Details
| Originalsprache | Englisch |
|---|---|
| Seiten (von - bis) | 49-67 |
| Seitenumfang | 19 |
| Fachzeitschrift | Procedia CIRP |
| Jahrgang | 6 |
| Ausgabenummer | 1 |
| Frühes Online-Datum | 9 Aug. 2014 |
| Publikationsstatus | Veröffentlicht - März 2015 |
Abstract
To address the challenges of future air traffic, such as more accessible air travel with better public acceptance, this research work focuses on efficient active high-lift systems (AHLS). This system applies boundary layer suction combined with a controlled Coanda jet. Electrically powered compressors are located in the wings at each flap to supply the suction and blowing air mass flow rate to the AHLS, thus coupling the two in a useful way. This concept provides flexibility and controllability of lift generation and is consistent with the trend towards an “all-electric aircraft”. General models for assessment of such systems in preliminary aircraft design are not available yet as they require interdisciplinary expertise. This paper provides general design considerations for the components of this type of electrically powered AHLS, comprising compressors, motors, power electronics, system peripherals, and generators. The conceptual design for those components results in models for preliminary aircraft design which allows estimating power consumption, size and mass.
ASJC Scopus Sachgebiete
- Sozialwissenschaften (insg.)
- Verkehr
- Ingenieurwesen (insg.)
- Luft- und Raumfahrttechnik
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in: Procedia CIRP, Jahrgang 6, Nr. 1, 03.2015, S. 49-67.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - Design considerations for the components of electrically powered active high-lift systems in civil aircraft
AU - Teichel, S. H.
AU - Dörbaum, M.
AU - Misir, O.
AU - Merkert, A.
AU - Mertens, A.
AU - Seume, J. R.
AU - Ponick, B.
N1 - Funding information: The authors would like to thank the German Research Foundation (DFG) for supporting this research as part of the Collaborate Research Centre 880 (SFB 880).
PY - 2015/3
Y1 - 2015/3
N2 - To address the challenges of future air traffic, such as more accessible air travel with better public acceptance, this research work focuses on efficient active high-lift systems (AHLS). This system applies boundary layer suction combined with a controlled Coanda jet. Electrically powered compressors are located in the wings at each flap to supply the suction and blowing air mass flow rate to the AHLS, thus coupling the two in a useful way. This concept provides flexibility and controllability of lift generation and is consistent with the trend towards an “all-electric aircraft”. General models for assessment of such systems in preliminary aircraft design are not available yet as they require interdisciplinary expertise. This paper provides general design considerations for the components of this type of electrically powered AHLS, comprising compressors, motors, power electronics, system peripherals, and generators. The conceptual design for those components results in models for preliminary aircraft design which allows estimating power consumption, size and mass.
AB - To address the challenges of future air traffic, such as more accessible air travel with better public acceptance, this research work focuses on efficient active high-lift systems (AHLS). This system applies boundary layer suction combined with a controlled Coanda jet. Electrically powered compressors are located in the wings at each flap to supply the suction and blowing air mass flow rate to the AHLS, thus coupling the two in a useful way. This concept provides flexibility and controllability of lift generation and is consistent with the trend towards an “all-electric aircraft”. General models for assessment of such systems in preliminary aircraft design are not available yet as they require interdisciplinary expertise. This paper provides general design considerations for the components of this type of electrically powered AHLS, comprising compressors, motors, power electronics, system peripherals, and generators. The conceptual design for those components results in models for preliminary aircraft design which allows estimating power consumption, size and mass.
KW - Civil aircraft design
KW - Electrical active high-lift system
KW - More electric aircraft
UR - http://www.scopus.com/inward/record.url?scp=84922737118&partnerID=8YFLogxK
U2 - 10.1007/s13272-014-0124-1
DO - 10.1007/s13272-014-0124-1
M3 - Article
AN - SCOPUS:84922737118
VL - 6
SP - 49
EP - 67
JO - Procedia CIRP
JF - Procedia CIRP
SN - 2212-8271
IS - 1
ER -